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非结构网格限制器研究

李芳 孙唯哲 刘鑫 徐金秀

李芳, 孙唯哲, 刘鑫, 徐金秀. 非结构网格限制器研究[J]. 航空动力学报, 2015, 30(9): 2151-2159. doi: 10.13224/j.cnki.jasp.2015.09.013
引用本文: 李芳, 孙唯哲, 刘鑫, 徐金秀. 非结构网格限制器研究[J]. 航空动力学报, 2015, 30(9): 2151-2159. doi: 10.13224/j.cnki.jasp.2015.09.013
LI Fang, SUN Wei-zhe, LIU Xin, XU Jin-xiu. Research on limiters of unstructured grid[J]. Journal of Aerospace Power, 2015, 30(9): 2151-2159. doi: 10.13224/j.cnki.jasp.2015.09.013
Citation: LI Fang, SUN Wei-zhe, LIU Xin, XU Jin-xiu. Research on limiters of unstructured grid[J]. Journal of Aerospace Power, 2015, 30(9): 2151-2159. doi: 10.13224/j.cnki.jasp.2015.09.013

非结构网格限制器研究

doi: 10.13224/j.cnki.jasp.2015.09.013
基金项目: 

国家重点基础研究发展计划(2014CB744100)

国家高技术研究发展计划(2012AA01A306)

详细信息
    作者简介:

    李芳 (1980-),女,山西长治人,助理研究员,博士,研究方向为高性能计算技术.

  • 中图分类号: V21;TN401

Research on limiters of unstructured grid

  • 摘要: 研究了6种限制器形式及其参数计算方法,其中新的自适应VenkatakrishnanM限制器能够根据当地流场特征自动调节参数从而实现不同区域不同特性.数值试验表明:非结构网格限制器对邻居集合选择方法较敏感,其中共面法比共点法精度高约15%;高马赫数时压缩型限制器比耗散型限制器计算精度高约10%~40%;参变量算法中,方向梯度法得到的流场比增量法平滑;自适应VenkatakrishnanM限制器能够模拟复杂超声速流动.

     

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    [2] 王兰.超燃冲压发动机整机非结构网格并行数值模拟研究[D].四川 绵阳:中国空气动力研究与发展中心,2007. WANG Lan.Parallel numerical simulations of the whole scramjet engine flowfields on unstructured grids[D].Mianyang Sichuan:China Aerodynamics Research and Development Center,2007.(in Chinese)
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出版历程
  • 收稿日期:  2014-01-16
  • 刊出日期:  2015-09-28

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